Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊. II, High-wing model C / Randy S. Hultberg, Julio Chu, and Waldo L. Dickens.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Hultberg, Randy S.
Corporate Authors:	Bihrle Applied Research, Inc, Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Other Authors:	Chu, Julio, Dickens, Waldo
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1980.
Series:	NASA contractor report ; NASA CR-3201.
Subjects:	Aerodynamic measurements. Private planes. Spin (Aerodynamics) Wind tunnel balances.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.26:3201
NAS 1.26:3201	Available Place a Hold